View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 65947U 26145.34172162 +.00000000 +00000-0 +17432-3 0 00008
2 65947 51.8997 21.6088 0000968 101.7616 258.3455 14.79933837 08
| Epoch (UTC): | 25 May 2026 08:12:04 |
| Eccentricity: | 0.0000968 |
| inclination: | 51.8997° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 21.6088° |
| argument of perigee: | 101.7616° |
| revolutions per day: | 14.79933837 |
| mean anomaly at epoch: | 258.3455° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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